CN204142100U - A kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern - Google Patents
A kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern Download PDFInfo
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- CN204142100U CN204142100U CN201320803146.0U CN201320803146U CN204142100U CN 204142100 U CN204142100 U CN 204142100U CN 201320803146 U CN201320803146 U CN 201320803146U CN 204142100 U CN204142100 U CN 204142100U
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- self adaptation
- adaptation base
- rubber pneumatic
- gasbag
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- 230000006978 adaptation Effects 0.000 title claims abstract description 39
- 230000005855 radiation Effects 0.000 title claims abstract description 17
- 238000007789 sealing Methods 0.000 claims description 13
- 238000010304 firing Methods 0.000 abstract description 15
- 230000035939 shock Effects 0.000 abstract description 9
- 238000000034 method Methods 0.000 abstract description 8
- 210000004712 air sac Anatomy 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 3
- 230000006835 compression Effects 0.000 abstract description 2
- 238000007906 compression Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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Abstract
The utility model relate to a kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, belong to guided missile launcher technical field.This self adaptation base adopts air sac type structure, bottom Flange joint to firing box.After missile erecting, utilize chassis tire automatic inflatable/air system or external charger, by self adaptation base loading line, to the inflation of self adaptation base, after having inflated, firing box lands, and is played a supporting role to firing box by base.Because self adaptation base is air sac type structure, adapt to the gradient piece of smooth land and random road roughness by self-deformation.In emission process, MISSILE LAUNCHING shock loading can be delivered to ground by self adaptation base, and, when impact loading is to self adaptation base, self adaptation base can be produced distortion by compression, can cushioning effect be played, reduce launch load to the impact characteristics on ground, improve the adaptability that guided missile is launched at the low specific pressure piece of smooth land.This gasbag-type self adaptation base has the compatibility to cold and hot radiation pattern.
Description
Technical field
The utility model relates to guided missile launcher technical field, be specifically related to a kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern.
Background technology
Truck-mounted missile model development have long-range, rapid, maximize development trend, missile overall dimensions, weight are increasing, and no matter large-scale guided missile adopts which kind of radiation pattern hot and cold, and launching shock load all greatly increases.If radiation pattern adopts vehicle transmitting platform to transmit launching shock load, very high request will certainly be proposed to the intensity of flat pad, increase the weight of flat pad, make the motor-driven hydraulic performance decline of vehicle transmitting platform; Launching shock load is passed to ground by flat pad, can cause land subsidence, thus causes emitter disturbance, affects launch stability.Need launching shock load to be directly passed to ground, even if effective transmission of load still can be realized when ground launch depression, and the piece of smooth land gradient, unevenness and low specific pressure characteristic can be adapted to.In order to address this problem, need a kind of self adaptation base of design badly, realizing the adaptability of MISSILE LAUNCHING to the piece of smooth land gradient, unevenness, low specific pressure characteristic.
Utility model content
(1) technical problem that will solve
For solving the adjustment to the launching level ground gradient, unevenness and low specific pressure characteristic that the medium-and-large-sized MISSILE LAUNCHING of prior art exists, the utility model provide a kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, to ensure the adaptability of Missile Launching Process to the piece of smooth land.
(2) technical scheme
In order to solve the problems of the technologies described above, the utility model provide a kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, described gasbag-type self adaptation base comprises: air bag cover plate 1, adpting flange 2, sealing ring 3, loading line 4, rubber pneumatic bag 5, and gas throttling valve 6, wherein, described rubber pneumatic bag 5 is axially symmetric structure, comprise symmetrical first 501 and second 502, described second 502 is S shape, one end of described loading line 4 is arranged on described first 501, and described gas throttling valve 6 is arranged on described loading line 4; Described air bag cover plate 1 is positioned at the top of described rubber pneumatic bag 5, and is connected by described adpting flange 2 with rubber pneumatic bag 5, and described adpting flange 2 is multiple, is evenly distributed on first 501 and second 502 of described rubber pneumatic bag 5; Described sealing ring 3 is multiple, is evenly distributed on described air bag cover plate 1 and described rubber pneumatic bag 5 first 501 and between described air bag cover plate 1 and second 502 of described rubber pneumatic bag 5.
Preferably, described adpting flange 2 is two, and one is positioned on first 501 of described rubber pneumatic bag 5, and another is positioned on second 502 of described rubber pneumatic bag 5.
Preferably, described sealing ring 3 is two, one between described air bag cover plate 1 and first 501 of described rubber pneumatic bag 5, another is between described air bag cover plate 1 and second 502 of described rubber pneumatic bag 5.
(3) beneficial effect
The utility model utilizes rubber pneumatic bag self-deformation to solve the adjustment of large-scale MISSILE LAUNCHING existence to the launching level ground gradient, unevenness and low specific pressure characteristic, ensure that the adaptability of Missile Launching Process to the piece of smooth land.
Accompanying drawing explanation
Fig. 1 is the structural representation of the gasbag-type self adaptation base of the utility model embodiment;
Fig. 2 is the axially symmetric structure schematic diagram of rubber pneumatic bag in the gasbag-type self adaptation base of the utility model embodiment.
Wherein, 1 air bag cover plate; 2 adpting flanges; 3 sealing rings; 4 loading lines; 5 rubber pneumatic bags 5; 501 first; 502 second; 6 gas throttling valves.
Detailed description of the invention
For making the purpose of this utility model, content and advantage clearly, below in conjunction with drawings and Examples, detailed description of the invention of the present utility model is described in further detail.
The utility model provides a kind of in truck-mounted missile Vertical Launch process, and what MISSILE LAUNCHING shock loading is passed to ground can the self adaptation base of compatible cold and hot radiation pattern, and guided missile can be provided the adaptability of the piece of smooth land gradient, unevenness, low specific pressure characteristic.
As shown in Figure 1, what the utility model embodiment provided a kind ofly can the gasbag-type self adaptation base of compatible cold and hot radiation pattern comprise: air bag cover plate 1, adpting flange 2, sealing ring 3, loading line 4, rubber pneumatic bag 5, and gas throttling valve 6, wherein, described rubber pneumatic bag 5 is axially symmetric structure, comprise symmetrical first 501 and second 502(as shown in Figure 2), described second 502 is S shape, one end of described loading line 4 is arranged on described first 501, and described gas throttling valve 6 is arranged on described loading line 4; Described air bag cover plate 1 is positioned at the top of described rubber pneumatic bag 5, and be connected fastening with rubber pneumatic bag 5 by described adpting flange 2, and ensureing that sealing ring 3 seals reliably, described adpting flange 2 is multiple, is evenly distributed on first 501 and second 502 of described rubber pneumatic bag 5; Described sealing ring 3 is multiple, is evenly distributed on described air bag cover plate 1 and described rubber pneumatic bag 5 first 501 and between described air bag cover plate 1 and second 502 of described rubber pneumatic bag 5.
In the present embodiment, described adpting flange 2 is two, and one is positioned on first 501 of described rubber pneumatic bag 5, and another is positioned on second 502 of described rubber pneumatic bag 5.
In the present embodiment, described sealing ring 3 is two, one between described air bag cover plate 1 and first 501 of described rubber pneumatic bag 5, another is between described air bag cover plate 1 and second 502 of described rubber pneumatic bag 5.
The utility model embodiment provide a kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, its course of work is as follows:
Base is connected to bottom firing box by adpting flange 2.Firing box can be pop-up guided missile firing box used, also can be the heat emission guided missile firing box used of not led gas-flow by row at the bottom of case, namely have the compatibility to cold and hot radiation pattern.In concrete use procedure, air bag cover plate 1 also can omit need not, directly rubber pneumatic bag 5 is fixed at the bottom of firing box, but must the sealing property of sealing ring 3 be ensured.When after missile erecting, utilize chassis tire automatic inflatable/air system or external charger, by loading line 4, inflate to rubber pneumatic bag 5, after having inflated, close gas throttling valve 6, gasbag-type self adaptation base lands along with firing box, is played a supporting role to firing box by gasbag-type self adaptation base.Main force support structure due to gasbag-type self adaptation base is rubber pneumatic bag formula 5, and when launching level ground exists the gradient or launching level ground ground not at ordinary times, rubber pneumatic bag 5 can self-deformation, adapts to the gradient piece of smooth land and random road roughness.In Missile Launching Process, MISSILE LAUNCHING shock loading can be delivered to ground by self adaptation base, when impact loading is to rubber pneumatic bag 5, the internal gas of rubber pneumatic bag 5 is compressed produces distortion, cushioning effect can be played, reduce launch load to the impact characteristics on ground, improve the adaptability that guided missile is launched at the low specific pressure piece of smooth land.The utility model is applicable in Missile Launching Process, and MISSILE LAUNCHING shock loading is passed to ground.This self adaptation base is applicable to truck-mounted missile Vertical Launch, and chassis tire automatic inflatable/air system inflation can be utilized also can to utilize other external charger inflations.
As can be seen from the above embodiments, this self adaptation base adopts air sac type structure, bottom Flange joint to firing box.After missile erecting, utilize chassis tire automatic inflatable/air system or external charger, by self adaptation base loading line, to the inflation of self adaptation base, after having inflated, firing box lands, and is played a supporting role to firing box by self adaptation base.Because self adaptation base is air sac type structure, the gradient piece of smooth land and random road roughness can be adapted to by self-deformation.In emission process, MISSILE LAUNCHING shock loading can be delivered to ground by self adaptation base, and, when impact loading is to self adaptation base, self adaptation base can be produced distortion by compression, can cushioning effect be played, reduce launch load to the impact characteristics on ground, improve the adaptability that guided missile is launched at the low specific pressure piece of smooth land.This gasbag-type self adaptation base can by Flange joint to pop-up mode firing box or by bottom row lead gas-flow heat emission mode firing box, there is the compatibility to cold and hot radiation pattern.
The above is only preferred embodiment of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model know-why; can also make some improvement and distortion, these improve and distortion also should be considered as protection domain of the present utility model.
Claims (3)
1. one kind can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, it is characterized in that, described gasbag-type self adaptation base comprises: air bag cover plate (1), adpting flange (2), sealing ring (3), loading line (4), rubber pneumatic bag (5), and gas throttling valve (6), wherein, described rubber pneumatic bag (5) is axially symmetric structure, comprise symmetrical first (501) and second (502), described second (502) are S shape, one end of described loading line (4) is arranged on described first (501), described gas throttling valve (6) is arranged on described loading line (4), described air bag cover plate (1) is positioned at the top of described rubber pneumatic bag (5), and be connected by described adpting flange (2) with rubber pneumatic bag (5), described adpting flange (2), for multiple, is evenly distributed on first (501) and second (502) of described rubber pneumatic bag (5), described sealing ring (3) for multiple, be evenly distributed on described air bag cover plate (1) and described rubber pneumatic bag (5) first (501) and between described air bag cover plate (1) and second (502) of described rubber pneumatic bag (5).
2. as claimed in claim 1 can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, it is characterized in that, described adpting flange (2) is two, one is positioned on first (501) of described rubber pneumatic bag (5), and another is positioned on second (502) of described rubber pneumatic bag (5).
3. as claimed in claim 1 or 2 can the gasbag-type self adaptation base of compatible cold and hot radiation pattern, it is characterized in that, described sealing ring (3) is two, one is positioned between described air bag cover plate (1) and first (501) of described rubber pneumatic bag (5), and another is positioned between described air bag cover plate (1) and second (502) of described rubber pneumatic bag (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320803146.0U CN204142100U (en) | 2013-12-09 | 2013-12-09 | A kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320803146.0U CN204142100U (en) | 2013-12-09 | 2013-12-09 | A kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern |
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| Publication Number | Publication Date |
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| CN204142100U true CN204142100U (en) | 2015-02-04 |
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| CN201320803146.0U Expired - Lifetime CN204142100U (en) | 2013-12-09 | 2013-12-09 | A kind of can the gasbag-type self adaptation base of compatible cold and hot radiation pattern |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112945029A (en) * | 2021-01-29 | 2021-06-11 | 哈尔滨工业大学 | Flexible clamping tool based on inflation deformation |
| CN112945030A (en) * | 2021-01-29 | 2021-06-11 | 哈尔滨工业大学 | Arc-shaped flexible support bracket of hypersonic cruise missile |
-
2013
- 2013-12-09 CN CN201320803146.0U patent/CN204142100U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112945029A (en) * | 2021-01-29 | 2021-06-11 | 哈尔滨工业大学 | Flexible clamping tool based on inflation deformation |
| CN112945030A (en) * | 2021-01-29 | 2021-06-11 | 哈尔滨工业大学 | Arc-shaped flexible support bracket of hypersonic cruise missile |
| CN112945030B (en) * | 2021-01-29 | 2024-04-05 | 哈尔滨工业大学 | Arc-shaped flexible support bracket of hypersonic cruise missile |
| CN112945029B (en) * | 2021-01-29 | 2024-05-03 | 哈尔滨工业大学 | Flexible dress card frock based on inflation deformation |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20150204 |
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| CX01 | Expiry of patent term |